View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 46326U 26145.58335647 +.00000000 +00000-0 +84161-3 0 00006
2 46326 53.0337 308.0255 0007797 258.8604 358.3145 15.93320315 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007797 |
| inclination: | 53.0337° |
| perigee height: | 288 km |
| apogee height: | 298 km |
| right ascension of ascending node: | 308.0255° |
| argument of perigee: | 258.8604° |
| revolutions per day: | 15.93320315 |
| mean anomaly at epoch: | 358.3145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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